syscom3
Pacific Historian
Your thoughts. Can it be done?
Theres nothing too complicated about the Skyraider airframe. It could have easily been designed in 1941. The R-2800 was available in 1941 so that would not be a show stopper.
Compare the R-2800 to the R-3350 that was installed on the Skyraider in 1945. Both are of the same approximate weight, diameter and horsepower.
You think the Skyrider could have been combat ready in 1942 with a proven capability to carry a payload of 4000 lbs? I know the R2800 was quite thirsty for fuel, but if you're only talking about a 300 mile combat radius, perhaps this is not a factor.
R-2800
* Power output: 2,100 hp (1,567 kW) @ 2,700 rpm
* Specific power: 0.75 hp/in³ (34.1 kW/L)
* Power-to-weight ratio: 0.89 hp/lb (1.46 kW/kg)
* Diameter: 52.8 in (1,342 mm)
* Dry weight: 2,360 lb (1,073 kg)
R-3350
* Power output: 2,200 hp at 2,800 rpm (takeoff power)
* Specific power: 0.66 hp/in³
* Power-to-weight ratio: 0.82 hp/lb
* Diameter: 55.78 in (1,420 mm)
* Dry weight: 2,670 lb (1,212 kg)
Theres nothing too complicated about the Skyraider airframe. It could have easily been designed in 1941. The R-2800 was available in 1941 so that would not be a show stopper.
Compare the R-2800 to the R-3350 that was installed on the Skyraider in 1945. Both are of the same approximate weight, diameter and horsepower.
You think the Skyrider could have been combat ready in 1942 with a proven capability to carry a payload of 4000 lbs? I know the R2800 was quite thirsty for fuel, but if you're only talking about a 300 mile combat radius, perhaps this is not a factor.
R-2800
* Power output: 2,100 hp (1,567 kW) @ 2,700 rpm
* Specific power: 0.75 hp/in³ (34.1 kW/L)
* Power-to-weight ratio: 0.89 hp/lb (1.46 kW/kg)
* Diameter: 52.8 in (1,342 mm)
* Dry weight: 2,360 lb (1,073 kg)
R-3350
* Power output: 2,200 hp at 2,800 rpm (takeoff power)
* Specific power: 0.66 hp/in³
* Power-to-weight ratio: 0.82 hp/lb
* Diameter: 55.78 in (1,420 mm)
* Dry weight: 2,670 lb (1,212 kg)